What was found
DISCREPANCY: R BLEED OFF DURING CLIMB AFTER ENG ICE ON. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENGINE INLET THERMAL ANTI-ICE VALVE AS PER AMM 30-21-03. OPERATIONAL TEST NORMAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DISCREPANCY: R BLEED OFF DURING CLIMB AFTER ENG ICE ON. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENGINE INLET THERMAL ANTI-ICE VALVE AS PER AMM 30-21-03. OPERATIONAL TEST NORMAL.